View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 39265U 26145.57859170 +.00000000 +00000-0 +36613-3 0 00000
2 39265 80.9139 94.1300 0299417 138.2090 224.2438 15.23225942 09
| Epoch (UTC): | 25 May 2026 13:53:10 |
| Eccentricity: | 0.0299417 |
| inclination: | 80.9139° |
| perigee height: | 290 km |
| apogee height: | 702 km |
| right ascension of ascending node: | 94.1300° |
| argument of perigee: | 138.2090° |
| revolutions per day: | 15.23225942 |
| mean anomaly at epoch: | 224.2438° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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